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C210

From SKYbrary Wiki
Aircraft
Name 210 Centurion
Manufacturer CESSNA
Body Narrow
Wing Fixed Wing
Position High wing
Tail Regular tail, low set
WTC Light
APC A
Type code L1T
Engine Piston
Engine count Single
Position Nose mounted
Landing gear Tricycle retractable
Mass group 1


Manufacturered as:

AVIONES COLOMBIA 210
CESSNA Turbo Centurion
CESSNA T210 Turbo Centurion
CESSNA 210 Centurion
CESSNA 210
CESSNA Centurion


CESSNA 210 Centurion

CESSNA 210 Centurion

Description

High performance light aircraft. In service since 1960. Exists in several versions with different engines. Has been constantly updated but production of the basic version ceased in 1985. The P210 is the high performance pressurized type. Note: Similar to CESSNA 206 but with retractable gear and without wingstruts.

Technical Data

Wing span 11.2 m36.745 ft
Length 8.6 m28.215 ft
Height 3 m9.843 ft
Powerplant 210: 1 x 300 HP Continental IO-520L piston engine with 3 blade propeller.

T210: 1 x 310 HP Continental TSIO-520R turbocharged piston engine with 3 blade propeller.

Engine model Continental O-520

Performance Data

Take-Off Initial Climb
(to 5000 ft)
Initial Climb
(to FL150)
Initial Climb
(to FL240)
MACH Climb Cruise Initial Descent
(to FL240)
Descent
(to FL100)
Descent (FL100
& below)
Approach
V2 (IAS) 70 kts IAS 100 kts IAS 140 kts IAS 140 kts MACH TAS 170 kts MACH IAS 170 kts IAS kts Vapp (IAS) 75 kts
Distance 400 m ROC 500 ft/min ROC -500 ft/min ROC ft/min ROC ft/min MACH ROD ft/min ROD 500 ft/min MCS kts Distance 450 m
MTOW 18201,820 kg
1.82 tonnes
kg
Ceiling FL270 ROD ft/min APC A
WTC L Range 800800 nm
1,481,600 m
1,481.6 km
4,860,892.392 ft
NM

Accidents & Serious Incidents involving C210

None on SKYbrary